T4-95 Flow Past a Fin
(Europe)
Brief Description
The test is proposed to assess codes for simulating 3D supersonic
shock-wave / boundary-layer turbulent interaction around an unswept
fin/plate configuration with a blunt leading edge. Transition is
triggered ahead of the obstacle's leading edge.
Focal Point
- Numerical
Borsi (fax) +39-11-7181078
- Experimental
Barberis (fax) +33-1-46235061
Full Description
- Preview
full problem description Postscript document.
- Retrieve
compressed Postscript document.
Working Group Chairman
Francesco Grasso
Universita di Roma 'la Sapienza'
Dipartimento di Meccanica e Aeronautica
Via Eudossiana 18, Roma, Italia, 00184
(tel) +39-6-44585202 (fax) +39-6-4881759
e-mail: grasso@grasso.ing.uniroma1.it
Date of last change: July 13, 1995
hsff@math.uh.edu